초록 ▼

The invention relates to a housing system (10) for an axial turbomachine, in particular for an aircraft turbine, comprising a housing (12), at least one guide blade (14), which is fastened to the housing (12) by means of at least one fastening element (18),a scaling element (20) for reducing a leaka

The invention relates to a housing system (10) for an axial turbomachine, in particular for an aircraft turbine, comprising a housing (12), at least one guide blade (14), which is fastened to the housing (12) by means of at least one fastening element (18),a scaling element (20) for reducing a leakage flow between the listening element (18) and the housing (12), wherein the sealing element (20) is arranged between a downstream wall (22) of the fastening element (18) with respect to a flow direction (I) of the axial turbomachine and a wall (24) of the housing (12), and a pressing means (36), by means of which an axial force can be applied to the scaling element (20) And the scaling element can be pressed against the wall (24) of the housing (12), at least during the operation of the axial turbomachine. The invention further relates to an axial turbomachine having such a housing system (10).

대표청구항 ▼

1. A housing system for an axial turbomachine having a defined direction of flow, the housing system comprising: a housing including a first wall portion configured as a receptacle facing downstream relative to the direction of flow anda second wall portion disposed downstream relative to the direct

1. A housing system for an axial turbomachine having a defined direction of flow, the housing system comprising: a housing including a first wall portion configured as a receptacle facing downstream relative to the direction of flow anda second wall portion disposed downstream relative to the direction of flow from the first wall portion and facing upstream relative to the direction of flow;at least one vane that is fastened on the housing by at least one fastening element, the fastening element including a hook-shaped portion extending upstream relative to the direction of flow and configured to be received in the downstream-facing receptacle of the first wall portion of the housing,a first wall of the fastening element facing downstream relative to the direction of flow anda pressure edge portion bordering the first wall of the fastening element and facing downstream relative to the direction of flow; anda sealing element having a radially outer end disposed between the downstream-facing first wall of the fastening element and the upstream-facing second wall portion of the housing;whereby the housing, vane and sealing element define a first air chamber disposed upstream from the fastening element with a relatively high pressure therein during the operation of the turbomachine and a second air chamber disposed downstream from the fastening element with a relatively low pressure therein during the operation of the turbomachine;whereby the pressure edge portion of the fastening element is in contact with the sealing element and loads the sealing element with an axial force at least during the operation of the turbomachine so that the radially outer end of the sealing element is pressed against the upstream-facing second wall portion of the housing wall of the housing; andwhereby the sealing element reduces leakage flow between the fastening element and the housing; andwherein the sealing element further comprises at least one metering bore formed therethrough, by means of which a flow of cooling air can be adjusted between the first air chamber of the housing system that is disposed upstream from the fastening element and the second air chamber of the housing element that is disposed downstream from the fastening element. 2. A housing system for an axial turbomachine having a defined direction of flow, the housing system comprising: a housing including a first wall portion configured as a receptacle facing downstream relative to the direction of flow anda second wall portion disposed downstream relative to the direction of flow from the first wall portion and facing upstream relative to the direction of flow;at least one vane that is fastened on the housing by at least one fastening element, the fastening element including a hook-shaped portion extending upstream relative to the direction of flow and configured to be received in the downstream-facing receptacle of the first wall portion of the housing,a first wall of the fastening element facing downstream relative to the direction of flow anda pressure edge portion bordering the first wall of the fastening element and facing downstream relative to the direction of flow; anda sealing element having a radially outer end disposed between the downstream-facing first wall of the fastening element and the upstream-facing second wall portion of the housing;whereby the housing, vane and sealing element define a first air chamber disposed upstream from the fastening element with a relatively high pressure therein during the operation of the turbomachine and a second air chamber disposed downstream from the fastening element with a relatively low pressure therein during the operation of the turbomachine;whereby the pressure edge portion of the fastening element is in contact with the sealing element and loads the sealing element with an axial force at least during the operation of the turbomachine so that the radially outer end of the sealing element is pressed against the upstream-facing second wall portion of the housing wall of the housing; andwhereby the sealing element reduces leakage flow between the fastening element and the housing; andfurther comprising:a second wall of the fastening element facing downstream relative to the direction of flow and disposed on the fastening element such that the pressure edge portion is disposed between the first and second walls of the fastening element; anda groove formed on the second wall of the fastening element, within which groove a radially inner end of the sealing element is received. 3. A housing system in accordance with claim 2, wherein the groove on the second wall of the fastening element is offset in the upstream direction relative to the direction of flow with respect to the pressure edge portion of the fastening element. 4. A housing system for an axial turbomachine, the housing system comprising: a housing;at least one vane that is fastened on the housing by at least one fastening element;a sealing element for reducing a leakage flow between the fastening element and the housing, whereby the sealing element is arranged between a fastening element wall located downstream relative to a direction of flow of the axial turbomachine and between a wall of the housing; andwith a pressure feature by means of which the sealing element can be loaded with an axial force at least during the operation of the axial turbomachine and can be pressed against the wall of the housing; andwherein the sealing element comprises at least one through opening by means of which a flow of cool air can be adjusted between a first space of the housing system that is arranged upstream from the fastening element and a second space of the housing system that is arranged downstream from the fastening element. 5. A housing system for an axial turbomachine, the housing system comprising: a housing;at least one vane that is fastened on the housing by at least one fastening element;a sealing element for reducing a leakage flow between the fastening element and the housing, whereby the sealing element is arranged between a fastening element wall located downstream relative to a direction of flow of the axial turbomachine and between a wall of the housing; andwith a pressure feature by means of which the sealing element can be loaded with an axial force at least during the operation of the axial turbomachine and can be pressed against the wall of the housing; andfurther comprising a groove provided on the fastening element in which a radially inner end area of the sealing element is arranged; andwherein the groove is configured so as to be oblique. 6. A housing system for an axial turbomachine, the housing system comprising: a housing;at least one vane that is fastened on the housing by at least one fastening element;a sealing element for reducing a leakage flow between the fastening element and the housing, whereby the sealing element is arranged between a fastening element wall located downstream relative to a direction of flow of the axial turbomachine and between a wall of the housing; andwith a pressure feature by means of which the sealing element can be loaded with an axial force at least during the operation of the axial turbomachine and can be pressed against the wall of the housing; andfurther comprising a groove provided on the fastening element in which a radially inner end area of the sealing element is arranged; andwherein the groove is configured so as to be offset relative to the pressure feature.